View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 52840U 26145.66668980 +.00000000 +00000-0 +14379-1 0 00004
2 52840 53.2153 41.4415 0001598 93.7991 75.1867 15.43112800 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001598 |
| inclination: | 53.2153° |
| perigee height: | 436 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 41.4415° |
| argument of perigee: | 93.7991° |
| revolutions per day: | 15.43112800 |
| mean anomaly at epoch: | 75.1867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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